View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 19826U 26161.10839174 +.00000000 +00000-0 +51161-4 0 00006
2 19826 82.9522 288.5383 0028701 269.6913 272.9105 13.72553545 03
| Epoch (UTC): | 10 June 2026 02:36:05 |
| Eccentricity: | 0.0028701 |
| inclination: | 82.9522° |
| perigee height: | 969 km |
| apogee height: | 1012 km |
| right ascension of ascending node: | 288.5383° |
| argument of perigee: | 269.6913° |
| revolutions per day: | 13.72553545 |
| mean anomaly at epoch: | 272.9105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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